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The Tronair 02-0234-0111 is a 2-Ton (4,000 lb) hydraulic aircraft tripod jack engineered to lift aircraft from the forward fuselage or main wing jacking points during maintenance, inspections, and ground operations. With a 34" (86.4 cm) closed height and 79" (200.7 cm) maximum extended height, it accommodates a range of aircraft fuselage and wing jacking point heights. The single-stage hydraulic design provides controlled lift and positive lock at any extension height. CE-marked for compliance with European aviation safety standards. OEM-specified for Cessna 150, 152, 172 and others. Also approved for Piper Aerostar, Chieftan and others.
Standard Features
- Hand pump with built-in pressure relief valve
- Threaded rams with improved handwheel-style safety nut
- Quick-rising center extension for rapid initial lift
- Easy-access filler/breather cap
- Heavy-duty wheels for easy maneuverability
- Hydraulic fluid: MIL-PRF-5606
- ¾" (2 cm) spherical radius cup jack pad
- CE marked
- Durable powder-coat finish (Tronair Blue)
Technical Specifications
- Rated Capacity: 4,000 lbs (1814 kg)
- Operating Temperature: −4°F to 122°F (−20°C to 50°C)
- Pressure Relief Setting: 2,500 + 250/−0 PSIG (172.4 + 17.2/−0 bar)
- Minimum Closed Height: 34" (86.4 cm)
- Maximum Height Obtainable: 79" (200.7 cm)
- Hydraulic Fluid: MIL-PRF-5606
- Jack Pad: ¾" (2 cm) spherical radius cup
- Finish: Durable powder coat (Tronair Blue)
Safety Features
- Ram Lock Nut: Prevents the lowering of the ram. The ram lock nut must be lowered as the aircraft is being lifted. Ram lock nuts must be kept within 2" of the stop while raising the aircraft.
- Lock Nut Retention Ring: Prevents the lock nut from being unscrewed from the second stage.
- Pressure Relief Valve: Prevents overload during raising operations.
Aircraft Applications
The 02-0234-0111 is OEM-approved for the following aircraft types:
- Cessna: 150, 152, 172, 177, 180 and 12 more
- Piper: Aerostar, Chieftan, Navajo
- Gulfstream: Aero Commander
- Fairchild/Dornier: Dornier 228-100/200
- Eurocopter: AS350 A-Star (High Skid Gear)
This list reflects aircraft for which the manufacturer has specifically approved this jack. Additional applications may be possible — always confirm jacking capacity, adapter requirements, and placement procedures with the aircraft maintenance manual before use.
Need your Tronair 02-0234-0111 2-ton tripod jack serviced, repaired, or load tested?
Pilot John is an authorized Tronair distributor and factory-authorized Tronair service center. Every jack ships new from our warehouse with Certificates of Conformance (CofC) and FAA Form 8130-3 documentation available at no additional cost. Need jack service, load-testing, or repair? Pilot John handles that too as an OEM-trained GSE service center. For more information or to request service, see our Service Center page, and see our article on why jack load testing matters. Pilot John also operates an ISO-17025 calibration center for all of your tooling and equipment calibration needs — learn more here.
| General Information | |
|---|---|
| Part # | 02-0234-0111 |
| Manufacturer | Tronair |
| NSN | 1730015533926 |
| Shipping Information | |
|---|---|
| Shipping Weight | 150 lbs. |
| Shipping Dimensions | 21 x 26 x 37 in. |
| Freight NMFC | 186600 |
| Schedule B | 8425420000 |
| ECCN | EAR99 |
| Spare Parts | |
|---|---|
| G-1300-44220 | Roll Pin |
| G-1311-01 | Lock Pin |
| HC-1683-02 | Cylinder |
| HC-1728 | Hand Pump |
| HJ-207 | Inner Center Tube |
| HJ-213 | Jack Pad |
| K-1165 | Wheel (Set) Kit |
| K-1938 | Locking Pin Kit |
| K-2513 | Cylinder Seal Kit (Post 11/1995, Monarch) |
| K-4539 | Cylinder Seal Kit (Post 11/1995, Power Packer) |
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AIRCRAFT COMPATIBILITY
| Compatible Aircraft* | |
|---|---|
| Cessna |
150
NOTE
This jack is used on the main landing gear. Two jacks per aircraft are required.
,
152
NOTE
This jack is used on the main landing gear. Two jacks per aircraft are required.
,
172
NOTE
This jack is used on the main landing gear. Two jacks per aircraft are required.
,
177
NOTE
This jack is used on the main landing gear. Two jacks per aircraft are required.
,
180
NOTE
This jack is used on the main landing gear. Two jacks per aircraft are required.
,
182
NOTE
This jack is used on the main landing gear. Two jacks per aircraft are required.
,
185
NOTE
This jack is used on the main landing gear. Two jacks per aircraft are required.
,
206
NOTE
This jack is used on the main landing gear. Two jacks per aircraft are required.
,
207
NOTE
This jack is used on the main landing gear. Two jacks per aircraft are required.
,
210
NOTE
This jack is used on the main landing gear. Two jacks per aircraft are required.
,
310
NOTE
This jack is used on the main landing gear. Two jacks per aircraft are required.
,
320
NOTE
This jack is used on the main landing gear. Two jacks per aircraft are required.
,
337 Skymaster
NOTE
This jack is used on the main landing gear. Two jacks per aircraft are required.
,
340
NOTE
This jack is used on the main landing gear. Two jacks per aircraft are required.
,
411
NOTE
This jack is used on the main landing gear. Two jacks per aircraft are required.
,
414
NOTE
This jack is used on the main landing gear. Two jacks per aircraft are required.
,
421
NOTE
This jack is used on the main landing gear. Two jacks per aircraft are required.
|
| Eurocopter | AS350 A-Star (High Skid Gear) |
| Fairchild/Dornier | Dornier 228-100/200 |
| General Atomics | Predator B |
| Gulfstream |
Aero Commander
NOTE
This jack is used on the main landing gear. Two jacks and two leg extensions (03-5400-0000) per aircraft are required.
|
| Piper |
Aerostar
NOTE
This jack is used on the main landing gear. Two main jacks are required per aircraft.
,
Chieftan
NOTE
This jack is used on the main landing gear. Two main jacks are required per aircraft.
,
Navajo
NOTE
This jack is used on the main landing gear. Two main jacks are required per aircraft.
|
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QUESTIONS & ANSWERS
The Tronair 02-0234-0111 2-Ton Hydraulic Tripod Jack is designed to safely lift light aircraft for maintenance and inspection tasks. It provides a stable, self-contained hydraulic lifting system that supports the aircraft’s weight during wheel, gear, and undercarriage servicing. This model is built for both hangar and ramp use, combining portability with reliability.
Constructed from high-strength steel, the jack features telescoping legs and safety locking mechanisms on both the ram and legs to ensure stability during lifting operations. The heavy-duty 4” wheels allow easy positioning, while a self-contained hydraulic reservoir minimizes maintenance needs. These design elements make the unit robust and long-lasting under demanding aviation environments.
The 2-ton tripod jack arrives fully assembled and ready to use. Before operation, users should remove all packaging materials, verify the fluid level in the reservoir, and inspect the jack for damage or corrosion. A proper pre-use check ensures safe and reliable operation during aircraft lifting procedures.
Operators must never extend the legs unequally or strike them to reposition the jack, as this can cause structural damage to the jack. The ram locking pin must always be engaged once the aircraft is raised, and tail or nose stands should be used for added stability. These precautions are critical to prevent aircraft tilting or jack collapse during servicing.
Tronair recommends a functional load test every 12 months, applying a test load equal to 110% of the rated capacity to verify structural and hydraulic integrity. Operators should also perform quarterly visual inspections for leaks, corrosion, and mechanical wear as part of routine preventative maintenance.
The jack should always be placed on a hard, level surface directly beneath the aircraft’s designated jack pad. The hydraulic ram must remain vertical at all times to ensure even load distribution. Operators should avoid uneven leg extensions or off-center placement, as these can lead to jack instability and equipment damage.
To install the optional 03-5400-0000 leg extension set, technicians must replace each leg individually while ensuring proper orientation – especially for the two-wheeled legs. After installation, the safety chain must be adjusted to match the increased height of the jack. Equal leg extension is required for safe and balanced lifting.
When lowering the aircraft, the ram locking pin must be retracted first, and the pump release valve opened slowly to prevent a sudden descent. The aircraft should remain level as all jacks are lowered simultaneously. Raising the ram slightly before removing the pin makes this process easier and prevents mechanical strain.
Tronair warrants the 02-0234-0111 jack to be free from material and manufacturing defects for a period of one year from the date of shipment. The warranty covers repair or replacement of defective parts but excludes wear components and damage caused by misuse or unauthorized modification. Replacement parts carry a 90-day warranty. All warranty service requires prior authorization and an RMA number.


